M3MSAT, 41605 (Decayed)
Orbit data source: Space-Track
M3MSAT, 41605 was a Canadian payload satellite in LEO that was launched on Wed, 22 Jun 2016 UTC via a PSLV-XL launch vehicle from the Sirharikota (SRI). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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41605 intel report (Beta)
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Identifier
Orbit
Country
CARelated business
Manufacturer
Honeywell/ComDev
Mission
Decayed Defense Communications
Bus & Motor
MMMS, Unknown motor
Mass
85 kg wet, 85 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.4 m
Radar Cross Section
0.660 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 5 months ago
TLE from 5 months ago
0 M3MSAT
1 41605U 16040G 25353.51682543 .11453613 24279-5 13983-3 0 9999
2 41605 97.0276 23.8359 0008747 238.4233 121.6219 16.49580729529740Epoch: 2025-12-19T12:24Z
TLE epoch observation values (Epoch: 2025-12-19T12:24:13.717Z)
Latitude
-0.00002°
Longitude
109.4219°
Altitude
146.709 km
Speed
7.816 km/s
True Right ascension
01h 35m 20s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
17:31:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
142.918 km
Perigee altitude
131.52 km
Semi-major axis
6,515.356 km
Eccentricity
0.00087
Inclination
97.0276°
RAAN
23.8359°
Arg. of periapsis
238.4233°
True anomaly
121.7072°
Mean anomaly
121.6219°
Eccentric anomaly
121.66456°
Mean motion
4.12701 °/min
Orbital period
87.23 mins
BSTAR
0.00013983
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Other satellites on launch #40 in the year 2016 (2016-06-22 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.M3MSAT Visibility
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
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| This satellite is decayed. |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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